Post-combustion device and method

ABSTRACT

The technical field is post-combustion noxious emissions reduction. A post-combustion apparatus  100  mixes noxious gases with a post-combustion gas fuel that burns in air at least at 1950° C., more preferably greater than 2,000° C. in a chamber that mixes the gases  330  and then ignites them on entry into a combustion expansion chamber  360  with a larger sectional surface area ensuring that there is no constriction of the exhaust system from that point in the process to avoid back-pressure. A collection vessel  460 , typically using a magnet and water trap is also provided that collects particulate and other magnetic and soluble matter from the exhaust stream.

TECHNICAL FIELD

The present invention relates to post-combustion processing and more particularly to post-combustion processing using a combustible gas mixture.

BACKGROUND ART

There are many industries that combust materials, either to produce energy or to get rid of waste. The combustion process produces furnace exhaust gas that can have unacceptable concentrations of toxic chemicals and greenhouse gases, both of which are damaging to the environment.

Post-combustion technology has arisen as a way to partially address this issue. For example, U.S. Pat. No. 4,820,500 by Obermuller (incorporated in its entirety herein by reference), describes combusting a flammable gas in the presence of air with furnace exhaust gas. This process is conducted at relatively low temperatures and this teaches that the production of CO and NOx gases are undesirable. The process does result in a more complete burn of the gases, but also causes the release of toxic gases (depending on the nature of the furnace exhaust gas).

WO2015/015447 by Futurenergy Pty Ltd (Futurenergy) (incorporated in its entirety herein by reference), describes a combustion system using Magnegas, as described in U.S. Pat. No. 6,663,752. Unfortunately, the Futurenergy device is not suitable for long-term continuous usage, as would be required in any continuous furnace operation. Anything beyond short-term usage of the device described in the Futurenergy specification results in intermittent failure of post-combustion and decreasing efficiency that shuts down the combustion process. This can be explosively dangerous and damaging to the equipment. Intermittent failure also results in the undesirable release of unprocessed combustion gases into the environment.

Nothing above should be read as necessarily falling within the common general knowledge.

It would be desirable to produce a device that at least partially overcomes the above-mentioned disadvantages or that at least provides the public with a useful choice.

Definitions

In this specification, unless the context indicates otherwise:

-   -   a) “AS” means Australian Standard;     -   b) “furnace exhaust gas” is exhaust gas (including any         particulates) produced by a furnace. Typically furnace exhaust         gas is conventionally exhausted via a flue stack to the         atmosphere or post-processing equipment;     -   c) “connected” means directly connected as well as indirectly         connected;     -   d) “cross section” or variants like “cross sectional” in         relation to an area refers the area defined by internal space in         a section through an object at right angles to the direction of         usual gas flow.     -   e) “comprise”, or variations such as “comprises” or         “comprising”, will be understood to imply the inclusion of a         stated element, integer or step, or group of elements, integers         or steps, but not the exclusion of any other element, integer or         step, or group of elements, integers or steps;     -   f) “chamber” means an enclosed space or cavity that is         optionally connected to other chambers, ducts or passageways.         This definition also encompasses multiple chambers that, in use,         function as a single unit;     -   g) “cooler” means a container, vessel, or apparatus for cooling,         such as a heat exchanger,     -   h) “mode” in a statistical sense refers to the most frequently         occurring number found in a set of numbers. The mode is found by         collecting and organizing the data in order to count the         frequency of each result. For the purposes of the present         specification, measurements are rounded to the nearest 5         millimetres;     -   i) “K” is an symbol for temperature expressed in kelvin;     -   j) “g” is grams;     -   k) “mg” is milligrams (10⁻³ grams);     -   l) “min” is minute or minutes, depending on context;     -   m) “centrifugal compressor” is a compressor wherein energy is         transferred from a set of rotating impeller blades to a gas. The         gas flow is radial, and the energy transfer is caused from a         change in the centrifugal forces acting on the gas;     -   n) “T304L” is a type of stainless steel material well-known in         the fabrication industry having non-ferrous components of         Chromium 17-20%, Nickel 8-10.5%, Carbon up to a maximum of         0.03%, Magnesium up to 2%, Silicon up to 0.75%, Phosphorus up to         0.045%, and Sulphur up to 0.03%;     -   o) “SCH10” is a standard pipe size per ASME/ANSI B 36.10 “Welded         and Seamless Wrought Steel Pipe”;     -   p) “NB” is a nominal bore (inner diameter) expressed in mm;     -   q) “Nm³” is gas volume in dry cubic metres at standard         temperature and pressure (0° C. and 101.3 kPa);     -   r) “CO” is carbon monoxide;     -   s) “CO₂” is carbon dioxide;     -   t) “NOx” is a combined term for molecules containing one         nitrogen and one or more oxygen atom, such as NO and NO₂;     -   u) “PM” is particulate matter,     -   v) “H₂S” is hydrogen sulphide;     -   w) “STP” means standard temperature and pressure (0° C. and         101.3 kPa)     -   x) “VOC” is a chemical compound based on carbon chains or rings         with a vapour pressure greater than 0.01 kPa at 293.15 K (i.e.         20° C.) that participate in atmospheric photochemical reactions.         The following compounds are excluded from the definition: carbon         monoxide; methane; acrylamide; benzene hexachloro; biphenyl;         chlorophenols; n-dibutyl phthalate; ethylene glycol;         di-(2-ethylhexyl) phthalate (DEHP); 4,4-methylene bis 2,4         aniline (MOCA); Methylenebis; Phenol; and         toluene-2,4-diisocyanate.     -   y) “TVOC” is a grouping of a wide range of VOC to simplify         reporting when these are present in ambient air or emissions. In         measuring TVOC in the present invention, such substances must be         present in polluted air, that is, vapours of gases given off by         compounds rather than the liquid phase;     -   z) “TVOC (propane)” means TVOC measured using a sensor         calibrated using propane;     -   aa) “reducer” is a component in a pipeline that reduces the pipe         size from a larger to a smaller bore (inner diameter). The         length of the reduction is usually equal to the average of the         larger and smaller pipe diameters. There are two main types of         reducer: concentric and eccentric reducers. In the present         specification, concentric reducers are mainly used. A reducer is         independent of fluid flow direction, so a reducer can be used         with a reduced diameter upstream and an enlarged diameter         downstream;     -   bb) USEPA means United States Environmental Protection         Authority.

The art-skilled worker will appreciate that the above definitions can and should, with suitable consideration for context, apply to the singular and the plural, and also to the tense of verbs, nouns, adjectives and adverbs derived from the above terms.

SUMMARY OF INVENTION

In a first aspect, the present invention provides a post combustion apparatus comprising:

-   -   a) a furnace flue inlet that (in use) connects to a furnace and         permits ingress of furnace exhaust gas into the post combustion         apparatus, thereby defining (in use) an extreme upstream         location of furnace exhaust gas entering the apparatus;     -   b) a post combustion exhaust chamber comprising an inlet and an         outlet, the outlet defining (in use) the extreme downstream         location of processed furnace exhaust gas exiting the apparatus,         such that gas flows (in use) between said extreme upstream         location and said extreme downstream location;     -   c) a cooler comprising an inlet, connected to the furnace flue         inlet, an outlet and a cooling element;     -   d) a mixing chamber comprising an inlet, connected to the outlet         of the cooler, an outlet, and a post-combustion gas fuel         injection port located downstream of the mixing chamber inlet         that, in use, introduces and mixes post-combustion gas fuel with         furnace exhaust gas;     -   e) a non-return valve interposed between the cooler outlet and         the mixing chamber inlet, which non-return valve is configured         to permit the flow of gas substantially in one direction only         from the cooler to the mixing chamber;     -   f) a combustion expansion chamber comprising an inlet, connected         to the mixing chamber outlet, and an outlet connected to the         combustion exhaust inlet;     -   g) an igniter located downstream of the fuel injection port         within the mixing chamber or the combustion expansion chamber;     -   h) a gas power system connected to the post combustion apparatus         configured to, in use, drive furnace exhaust gas and         particulates from the furnace flue inlet downstream through the         post combustion apparatus and to the post combustion exhaust         outlet;     -   i) wherein a mode of cross-sectional combustion expansion         chamber area, bounded by internal walls of the combustion         expansion chamber perpendicular to the gas flow, is larger than         a mode of cross-sectional mixing chamber area, defined by         internal walls of the mixing chamber and exhaust perpendicular         to the gas flow; and     -   j) wherein a mode of a cross-sectional combustion exhaust         chamber area, bounded by internal walls of the combustion         exhaust chamber perpendicular to the gas flow, is larger than         the mode of cross-sectional mixing chamber area.

In a further aspect, the present invention provides a process of post combustion comprising the steps of:

-   -   a) feeding furnace exhaust gas through a furnace flue inlet from         a furnace that permits ingress of furnace exhaust gas into the         post combustion apparatus, thereby defining an extreme upstream         location of furnace exhaust gas entering the apparatus;     -   b) exhausting processed furnace exhaust gas from an outlet in a         post combustion exhaust chamber comprising an inlet and the         outlet, the outlet defining the extreme downstream location of         processed furnace exhaust gas exiting the apparatus, such that         gas flows between said extreme upstream location and said         extreme downstream location; c) feeding furnace exhaust gas into         a cooler comprising an inlet from the furnace flue inlet, an         outlet and a cooling element and cooling the furnace exhaust         gas;     -   d) feeding cooled furnace exhaust gas into a mixing chamber         comprising an inlet, connected to the outlet of the cooler, an         outlet, and a post-combustion gas fuel injection port located         downstream of the mixing chamber inlet and mixing the cooled         furnace exhaust gas with post-combustion gas fuel;     -   e) preventing backflow of gas by passing gas through a         non-return valve interposed between the cooler outlet and the         mixing chamber inlet, which non-return valve is configured to         permit the flow of gas substantially in one direction only from         the cooler to the mixing chamber,     -   f) passing the mixed cooled furnace exhaust gas and         post-combustion gas fuel into a combustion expansion chamber         comprising an inlet, connected to the mixing chamber outlet, and         an outlet connected to the combustion exhaust inlet;     -   g) igniting the mixed cooled furnace exhaust gas and         post-combustion gas fuel using an igniter located downstream of         the fuel injection port within the mixing chamber or the         combustion expansion chamber,     -   h) driving the gas in the post combustion process by use of a         gas power system connected to the post combustion apparatus that         drives gas from the furnace flue inlet downstream through the         post combustion apparatus and to the post combustion exhaust         outlet;     -   i) wherein the combusting cooled furnace exhaust gas and         post-combustion gas fuel mixture is free to expand through the         combustion expansion chamber due to the combustion expansion         chamber having a mode of cross-sectional combustion expansion         chamber area, bounded by internal walls of the combustion         expansion chamber perpendicular to the gas flow, is larger than         a mode of cross-sectional mixing chamber area, defined by         internal walls of the mixing chamber and exhaust perpendicular         to the gas flow; and     -   j) wherein the combusted cooled furnace exhaust gas and         post-combustion gas fuel mixture is free to exit the combustion         expansion chamber due to the combustion expansion chamber having         a mode of a cross-sectional combustion exhaust chamber area,         bounded by internal walls of the combustion exhaust chamber         perpendicular to the gas flow, is larger than the mode of         cross-sectional mixing chamber area.

In relation to both of the above aspects:

Preferably, the ratio of the mode of cross-sectional area of the combustion expansion chamber is greater than that of the mode of cross-sectional area of the mixing chamber, more preferably at least double that of the mode of cross-sectional area of the mixing chamber.

It is also preferred for the mode of a cross-sectional combustion exhaust chamber area to be at least double that of the mode of the mixing chamber area.

The combustion exhaust chamber outlet can be connected to an exhaust flue stack. In a currently preferred embodiment, the combustion exhaust chamber is connected to an inlet for the furnace such that, in use, at least some processed furnace exhaust gas is recycled into the furnace. Preferably, the amount of processed furnace exhaust gas entering the furnace is controlled by way of a valve.

It is particularly preferred that the minimum cross-sectional area anywhere along the combustion expansion chamber through to the outlet of the apparatus is greater than the mean cross-sectional area of the mixing chamber.

Oxygen levels in the mixing chamber should be below atmospheric levels. The inventors have found that high levels of oxygen in the mixing chamber often cause the post-combustion gas fuel to undesirably react preferentially with oxygen. It is preferred that the post-combustion gas fuel be allowed to react with the furnace emissions. The exhaust path between the furnace and the exhaust stack should preferably be sealed from the air and no additional oxygen should be introduced into the system.

The exhaust path should preferably be at least the same cross-sectional area as the expansion chamber to minimise back-pressure. Back pressure has been found to degrade the performance of the post-combustion apparatus and process.

In a further preferred embodiment, at least some processed furnace exhaust gas is used as a heat source for generators, preferably by way of a steam-line heat exchanger.

For best results, furnace exhaust gas is preferably cooled to between 360 K and 395 K by the cooler. In a currently preferred embodiment, the cooler comprises a pre-combustion water jacket, preferably supplied by a compressor pump with water as a cooling medium. Optionally, water heated during the cooling process is fed to a steam generator. More preferably, the steam is cooled to liquid water and recycled.

Preferably, the mixing chamber is between 0.3 m and 1.5 m in length, more preferably 0.8 m to 1.5 m in length. Preferably, the post-combustion gas fuel injection port has at least one nozzle within the chamber, more preferably angled to swirl post-combustion gas fuel at least partially radially perpendicular to the flow direction of the furnace exhaust gas. In a currently preferred embodiment, there are three post-combustion gas fuel injection ports, preferably spaced 0.1-0.3 m apart, more preferably 0.2 m apart and extending in the direction of propagation of the furnace exhaust gas.

The distance from the nozzle closest to the combustion furnace is to be located sufficiently far from the cooler to ensure that all of the furnace exhaust gas has been cooled and mixed sufficiently that no furnace exhaust gas in proximity to the nozzle is above the post-combustion gas ignition temperature, more preferably no greater than 395 K.

The distance from the nozzle nearest to the combustion expansion chamber should be sufficient distance away from it to efficiently mix the post-combustion gas fuel and cooled furnace exhaust gas prior to combustion taking place.

Further nozzles can be supplied to optimise the inflow of post-combustion gas fuel and to maximise the mixing of the gases. The nozzles are preferably angled to swirl the post-combustion gas fuel in the general downstream direction. In one embodiment, a minority of the nozzles (it could be a single nozzle) is directed in a direction oblique to the other nozzles to impart turbulence.

Preferably, the angle of the nozzles is capable of being varied depending on the volume, density and composition of the cooled furnace exhaust gas being mixed with the Post-combustion gas. It is currently preferred that the optimum burning be judged by an increasing roaring sound emanating from the post combustion reaction and the nozzles manually adjusted to achieve optimum burning.

A suitable post-combustion gas fuel will largely depend on the nature of the emissions from the fuel being burned in the furnace. That is a function of the furnace itself and the type of fuel being burned in the furnace. For most practical purposes, the post-combustion gas fuel is a gas capable of combustion in air with an air flame temperature of at least 1,950° C. at STP. Non-limiting gases in this low temperature group include propane, butane, methane and propane-butane mixtures.

It is, however, more preferred for the post-combustion gas fuel to be a gas capable of combustion in air with an air flame temperature at STP of at least 2,000° C. for a better reaction. Non-limiting examples are a CO/H₂ mixture (Hydrogen 55-65% and carbon monoxide 30-35%), hydrogen, acetylene, propane, cyanogen and dicyanoacetylene.

The inventors have found that the post-combustion process is most efficient when the furnace exhaust gas is rich in TVOC, particulates and carbon monoxide emissions. It is therefore strongly preferred to have only a single post-combustion chamber in series with the furnace instead of a series of multiple combustion chambers. However, parallel configurations served by a manifold with multiple outlets for larger furnaces are contemplated.

Additionally, to prevent having to cool the furnace exhaust gas too much and to increase safety, the post-combustion gas fuel should preferably have an ignition temperature in air at STP greater than 480° C. Most preferably, the post-combustion gas fuel is a CO/H₂ mixture (Hydrogen 55-65% and carbon monoxide 30-35%) or hydrogen.

The non-return valve is preferably a swing gate check valve, but other valves are known in the industry that are suitable. Any valve chosen should have minimal resistance to opening and should be highly sensitive to backpressure, causing it to close as quickly as possible.

Preferably, a main flow control valve is interposed between the furnace flue inlet and the cooler or between the cooler and the mixing chamber to control the flow rate of the furnace exhaust gas through the gas post combustion apparatus. In a current embodiment, this is a manually-operated valve.

The combustion expansion chamber needs to withstand high temperatures. It is therefore preferably internally ceramic lined, more preferably cast ceramic lined. In a currently preferred embodiment, a Kaolin ceramic clay is employed.

The present invention is not limited to this embodiment as other methods and materials able to protect the chamber are available and known to art-skilled workers, especially those in the aerospace and furnace industries. Particularly preferred are ceramics employed in high-voltage ceramic power pole insulators that can withstand very high temperatures.

The igniter can be anything that raises the temperature of the mixture of gases to ignition point. Currently preferred are a pilot light, a spark plug, a series of spark plugs or combinations of these.

The igniter is preferably located proximal the inlet of the combustion expansion chamber. In a currently preferred embodiment, it is a sparkplug, more preferably a platinum spark plug connected to a 12 V transformer though an ignition coil generating continuous sparks. Art-skilled workers will be aware of this technology from the automotive industry. To ensure the best chance of obtaining continuous ignition, in one embodiment, multiple igniters can be used, preferably multiple spark plugs, most preferably 3 spark plugs. In addition, multiple ignition types can be used, such as spark plugs in conjunction with pilot lights.

The gas power system is preferably connected between the cooler and the mixing chamber. This permits the use of materials that do not need to tolerate the high temperatures of furnace exhaust gas prior to being cooled. Even so, the chosen materials need to realistically survive temperatures in excess of 580 K, so art-skilled workers will generally choose materials typically used in the gas turbine industry. In the currently preferred embodiment, the gas power system is an electric motor connected by belt to a centrifugal compressor incorporating an impeller.

In one embodiment, a matter collection chamber is installed between the combustion expansion chamber and the post combustion exhaust chamber, which matter collection chamber comprises a gas passage and a matter collection vessel. More preferably, the matter collection vessel has at least one magnet in close association with it that, in use, draws magnetised material out of the gas flowing through the gas passage into the matter collection vessel. The at least one magnet is preferably at least one electromagnet, more preferably a series of electromagnets. The series of electromagnets are preferably mounted on brackets located beneath mild steel plate. A series of electromagnets are powered by 240 V A/C mains power.

Conveniently, the matter collection vessel is located, in use, beneath the gas passage. In use, predominantly, the matter collection vessel preferably collects solid matter, more preferably activated carbon. The magnet should be kept relatively cool or it can stop working efficiently or become inoperative. The use of the combination of the water tray assists in keeping the magnets cool enough to function.

In one embodiment, matter collection vessel in a currently preferred embodiment also comprises a water tray between the exhaust flow and the electromagnets that retains particulates, such as activated carbon, in the water even after the electromagnets are turned off. This permits harvesting of particulates and the water also serves to cool the electromagnets.

In a currently preferred embodiment, a U-bend pipe is installed into the apparatus to change direction of flow, more preferably located before the matter collection chamber. The change of direction of flow increases the turbulence of the gas. An alternative option is to install vanes to induce turbulence prior to the matter collection chamber.

Water jackets are preferably installed between the combustion expansion chamber and the extreme downstream location such that the combusted cooled furnace exhaust gas and post-combustion gas fuel mixture is cooled within 2 seconds so that the gas exits the outlet of the apparatus at a temperature lower than 500° C. This assists in preventing the formation of noxious compounds of the dioxin and furan families.

BRIEF DESCRIPTION OF DRAWINGS

The invention is described below with reference to non-limiting examples as illustrated by the drawings, wherein:

FIG. 1 is a perspective view of a post-combustion apparatus of the invention;

FIG. 2 is a perspective view of a post-combustion apparatus of the invention in conjunction with a furnace;

FIG. 3 is a sectional side view of a portion of the post combustion apparatus of FIG. 1;

FIG. 4 is a sectional side view of a mixing chamber in the post-combustion apparatus shown in FIG. 1;

FIG. 5 is a blown-up view of a nozzle identified as A-A in FIG. 4;

FIG. 6 is a sectional side view through valves located between a mixing chamber and impeller as shown in FIG. 3;

FIG. 7 is a perspective view of a non-return valve in the post-combustion apparatus shown in FIG. 1 with part of the supply pipe removed to expose the elements of the valve;

FIG. 8 is a perspective view of a matter collection chamber in the post-combustion apparatus shown in FIG. 1; and

FIG. 9 is a sectional side view of a matter collection chamber as shown in FIG. 7.

FIG. 10 is a graph of baseline measurements for various emissions from a furnace without being put through a post-combustion process.

FIG. 11 is a graph of measurements for various emissions from a furnace coupled with a post-combustion process.

DESCRIPTION OF EMBODIMENTS

The invention is described below with reference to examples. The examples are only preferred embodiments of one or more ways that the invention can be carried out and should not be read as limiting the scope of the claimed invention.

With reference to FIG. 1, a post combustion apparatus, generally indicated as 100 has a furnace flue inlet 110 connected to a furnace flue (not shown in FIG. 1) by way of a furnace flue flange 120. Furnace flue inlet 110 is an extreme upstream location of furnace exhaust gas entering the post combustion apparatus 100.

On the opposite side of post combustion apparatus 100 is a post combustion exhaust chamber 130 that has an inlet 140 and an outlet 150, the outlet 150 being the extreme downstream location of processed furnace exhaust gas exiting the apparatus. Gas flows (in use) from furnace flue inlet 110 to outlet 150.

There are also additional alternative exhaust outlets. Three generating connections 160, 170, 180 in use connect to generators (not shown).

Another alternative exhaust is via a furnace return 190, that in use, returns hot gas to a supplying furnace to aid in furnace efficiency. This connection is affected by way of a flange 200 and controlled by an interposed manual control valve 195.

A cooler 210 has an inlet, which is the furnace flue inlet 110, and an outlet 220. A water jacket 230 acts in use as a cooling element by pumping water via a water inlet 240 into the water jacket 230 and out of a water outlet 250 to a water compressor pump 260.

The compressor pump 260 is connected by a water line 270 to a water supply inlet 280. An electrical water pump 290 is connected between the water line 270 and water supply inlet 280. A manually operated valve 300 is interposed between the electrical water pump 290 and the water supply line 270.

A gas power system, generally indicated as 310, is a centrifugal impeller compressor pump that is connected to the cooler 210 via the outlet 220. An outlet 320 connects to a non-return valve, generally indicated as 325, that is, in turn connected to a mixing chamber 330.

The mixing chamber 330 has three post-combustion gas fuel injection ports 340 and an outlet 350. The mixing chamber 330 is 1.3 m in length.

The outlet 350 is connected to a combustion expansion chamber 360, in turn connected to a tubular heat exchanger 370 through an exhaust gas inlet 380. The heat exchanger 370 has an exhaust gas outlet 390, a steam line inlet 400 and a steam line outlet 410 connected to an exhaust steam line 411. Steam generator connection flanges 412, 415 and 417 permit connection of the exhaust steam line 411 to steam driven electrical generators (not shown).

The steam line inlet 400 is connected via a steam supply line 420 to the water compressor pump 260. The steam line inlet 400 is also connected via a water supply line 430 to a manually operated valve 440 connected to the water supply 280 via the electrical water pump 290.

A U-bend pipe 450 is connected to the exhaust gas outlet 390 at one end and a matter collection chamber 460 at the other end.

Throughout the drawings, connections between elements are typically achieved by way of complementary flanges that are connected together by nuts, bolts and washers in the usual way. These flanged connections are depicted in the drawings but are not necessarily numbered herein in the interests of decluttering the drawings.

With reference to FIG. 2, the post-combustion apparatus 100 as shown in FIG. 1 is shown connected to a furnace, generally indicated as 500. In the interests of succinctness, the reader is directed to the explanation of the reference numerals in relation to the post combustion apparatus 100 in FIG. 1, which have the same meanings in FIG. 2. Not all reference numerals shown in FIG. 1 are shown in FIG. 2 in the interests of decluttering FIG. 2.

The furnace 500 is a commercial incineration chamber furnace, model: Midi Waste Incinerator by Proburn Waste Incinerators. It has a conveyor 510 connected to a door 520, that permits entry of waste material for combustion (not shown) from the conveyor 510 into a furnace combustion chamber 530, in turn connected to a furnace exhaust chamber 540, in turn connected to a furnace flue 550.

The furnace flue 550 is connected to the furnace flue flange 120.

Furnace return pipes 560 and 570 are connected at one end thereof to the lower end of furnace combustion chamber 530. The furnace return pipes 560 and 570 are connected at the other end thereof to the furnace return 190 at the flange 200.

With reference to FIG. 3, a portion of the post combustion apparatus 100 is shown. Elements of the same numbers as appear in earlier figures are identical and are not re-described here. The reader is directed to the earlier description for these reference numerals.

The gas power system 310 has an impeller 600 driven by a pulley (not shown) connected via a belt 610 to an electric motor 620 The impeller is rated to at least 580 K. The impeller 600 is an Aerotech branded, Model HP 184 steel housed 500 mm impeller with a 120 mm diameter outlet and a 150 mm diameter inlet connected by a direct drive connected to a 415 volt 4 kW electric motor 620.

The outlet 320 connects to a reducer 630 that reduces the inner pipe diameter to 100 mm and is connected to the non-return valve 325. The non-return valve 325 consists of a swing gate check valve 640 in conjunction with a manually operated ball valve 650 for emergency cut-off.

The ball valve 650 is connected to the mixing chamber 330. The mixing chamber 330 is made from 100 mm NB SCH10 welded pipe T304L. The injection ports, generally indicated by 340, consist of 3 injectors 660, 670 and 680.

At the downstream end of the mixing chamber 330 is a reducer 690 that expands the inner diameter from 100 mm to 200 mm. On the reducer 690 is a platinum spark plug 700 igniter connected to a 12 V transformer though an ignition coil generating continuous sparks (not shown).

The reducer 690 opens into the combustion expansion chamber 360, which has a ceramic lining 710 of refractory ceramic. The ceramic lining 710 has a 200 mm NB and a lining thickness of between 40 to 48 mm.

The ceramic lining 710 is housed within 300 mm NB SCH10 T304L welded pipe 720, connected to 300×200 mm NB SCH10 T304L reducers 730, 740 at each end of the combustion expansion chamber 360.

The ceramic lining 710 is created by forming a mould by inserting a plastic pipe (not shown) with an outer diameter of 200 mm into the welded pipe 720, thereby forming a mould filling cavity. A pumping hole is formed in the one end of the plastic pipe (not shown). A castable high alumina low cement refractory powder (by weight: Al₂O₃ 84%, SiO₂ 7.5%, CaO 3.3%, Fe₂O₃ 1.3%, alkalies 0.23% and TiO₂ 1.5%) is mixed with water using an electric mixer to make up to 4.4-5.5% by weight water. This forms a pumpable slurry that is pumped through the pumping hole (not shown) to fill the mould (not shown). The pumping hole is sealed once the mould is filled. The mould is agitated until the ceramic is set. Once dry, the plastic pipe (not shown) is removed and gaps and cracks in the ceramic lining 710 are filled in using an air-setting refractory wet mortar (not separately shown) comprising by weight: Al₂O₃ 42%, Fe₂O₃ 0.7%, CaO(+MgO) 0.4%, SiO₂ 45%, alkalies 3.5% and TiO₂ 1.5%. The ceramic lining 710 is permitted to dry and is gradually heated to operational temperature and maintained there for a few hours prior to operational use.

The combustion expansion chamber 360 is connected to the heat exchanger 370 via the exhaust gas inlet 380.

The heat exchanger 370 has an exhaust gas passage 750 surrounded by 200 mm NB SCH10 welded pipe T304L. A water jacket 760 of tapered 300 mm NB SCH10 welded pipe T304L surrounds the exhaust gas passage 750. The water jacket 760 houses the steam line inlet 400 and the steam line outlet 410, in turn connected to the steam supply line 420 and the exhaust steam line 411, respectively.

The various parts of the post-combustion apparatus are supported on pipe supports 780, 790, 800, 810 and 820 that, in use, maintain the exhaust gas flow in a substantially horizontal plane. While these are shown in other drawings, they are not necessarily numbered in the interests of reducing clutter.

With reference to FIG. 3 and FIG. 4, the mixing chamber 330 is shown flanked by the ball valve 650 and the reducer 690 in FIG. 4 (both of which are only partially shown in this cut-away view).

The injection ports, generally indicated as 340, consist of the injectors 660, 670 and 680, each of which has angled nozzles 900, 910 and 920, respectively. The angled nozzles 900, 910 and 920 terminate into the mixing chamber 330 and can be swiveled within the mixing chamber 330 by the use of each of adjustment nuts 930, 940 and 950 (respectively) about gas-proof fittings 960, 970 and 980 (respectively). Angled nozzles 900 and 910 are drawn facing away from the point of view whereas nozzle 1000 is drawn facing laterally. Angled nozzles 900 and 910 are configured, in use to concentrically swirl the gas in the mixing chamber 330, whereas nozzle 1000 is configured to introduce turbulence to the gas in the mixing chamber 330.

The injectors 660, 670 and 680 are constructed from 25 mm NB SCH10 welded pipe T304L. The injectors 660, 670 and 680 are spaced 200 mm apart and are angled at 45° to the centreline of the chamber 330. A mixing length 990 is defined between the angled nozzle 900 and the end of the mixing chamber 330, which is about 0.48 m in length.

Nozzles 900, 910 and 920 are composed of metal, each having a reduced inner diameter of 10 mm at its terminus (only terminus 1000 is shown for nozzle 920, but the others are similarly configured).

With reference to FIG. 6 and FIG. 7, the non-return valve, generally indicated as 325, is shown, including the swing gate check valve 640 and the ball valve 650 connected between the gas power system outlet 320 and the mixing chamber 330. Swing gate check valve 640 and the ball valve 650 are independently operable.

The ball valve 650 has a handle 1100 connected to a ball 1110 in a seat 1125 that has a through bore 1120 that is shown in an open configuration that permits gas to pass through the ball valve 650. If the handle 1100 is rotated 90 degrees from that as shown, then the through bore 1120 will be occluded by the seat 1125 and the ball valve 650 will be in its closed configuration (not shown).

The swing gate check valve 640 has a hinge 1130 that hinges a sealing flap 1140 with a sealing plate 1150. The sealing plate 1150 has an orifice 1160. A connecting pipe 1170 (only partially shown in FIG. 7) connects the swing gate check valve 640 to the ball valve 650.

The sealing flap 1140 is substantially circular with a diameter of 91 mm whereas the orifice 1160 has a diameter of 92 mm. in use, the sealing flap 1140 is not able to swing back to a position upstream of the normal direction of the flow of emissions as it has been designed to seal against the sealing plate 1150.

The hinge 1130 is cut at a very slight diagonal which in a situation where there is no movement of gas causes the flap 1140 to close under its own weight. This is the same principle as described in US284084 to HICKEY, which is incorporated into this specification in its entirety by reference.

The flap 1140 will open as soon as the flow begins and will be held open by the flow. In the case of back pressure, the flap 1140 will close. Because the flap 1140 is sealing against the sealing plate 1150 (acting as a flange with a lesser diameter than the orifice 1160), the flap 140 is slightly smaller than the diameter of the connecting pipe 1170.

With reference to FIG. 8 and FIG. 9, the matter collection chamber 460 is installed between the U-bend pipe 450 and the combustion exhaust chamber inlet 140. A gas passage 1200 permits passage of gas between the U-bend pipe 450 and the combustion exhaust chamber inlet 140.

Three electromagnets 1210, 1220, 1230 that are 240V A/C Commercial Electro-Magnetic Base Power 13500N Magnetic Force from Techstyle group are located in a 6 mm material thickness stainless steel sealed enclosure 1240. A water tray 1250 is located beneath the gas passage 1200 that is supplied with a constant supply of water to replace water that is evaporated during operation.

In Use

With reference to the drawings, in use, the furnace 500 is fed by the conveyor 510 with waste material to be incinerated (not shown). The waste material (not shown) enters the furnace combustion chamber 530 via the door 520, where it is combusted.

Furnace exhaust gas (not shown) and particulates produced by the combustion pass up through the furnace exhaust chamber 540 and into the furnace flue 550. Furnace exhaust gas (not shown) passes into the post-combustion apparatus 100 via furnace flue inlet 110. Furnace flue inlet 110 is an extreme upstream location of furnace exhaust gas (not shown) entering the apparatus post combustion apparatus 100.

The furnace exhaust gas passes into the cooler 210, where it is cooled by the cooling jacket 230 by water pumped by water compressor pump 260 into the water inlet 240, which exchanges heat with the furnace exhaust gas and exits the cooling jacket 230 via the water outlet 250.

The compressor pump 260 equalises the pressure and level between the water lines. Water is driven via hot water outlet 250 by compressor pump 260 through a steam supply line 420 to the heat exchanger 370 steam line inlet 400.

For best results, the furnace exhaust gas is cooled to between 340 K and 395 K by the cooler 210. The cooled furnace exhaust gas is drawn into the gas power system 310 via the outlet 220.

The electric motor 620 drives the impeller 600 to draw cooled furnace exhaust gas through the gas power system from the cooler 210 and propel it onward via outlet 320.

The propelled cooled furnace exhaust gas passes through the reducer 630 and through the non-return valve 325.

In the case of a blow-back in the post-combustion apparatus 100, the swing gate check valve 640 closes by the upstream force of the blow-back causing sealing flap 1140 to hinge closed and seal against sealing plate 1150, preventing the return of the furnace exhaust gas back to the furnace via orifice 1160. Once blow-back pressure reduces to less than that created by the gas power system 310, sealing flap 1140 hinges open again by the pressure exerted by upstream furnace exhaust gas. Sealing flap 1140 is designed to be as light as possible while still allowing sufficient protection against blowback.

An emergency cut-off can also be effected by rotating the handle 1100 90° from its open position as depicted in FIG. 6 to its closed position, thereby isolating the post combustion apparatus downstream of the non-return valve 325.

The propelled cooled furnace exhaust gas enters the mixing chamber 330 and is mixed with a Post-combustion gas via the injection ports 340 supplied via the three injectors 660, 670 and 680 out of nozzles 900, 910, and 920 (respectively). The nozzles are angled to impart a swirling motion to the Post-combustion gas that assists in its mixing with the furnace exhaust gas.

The post-combustion gas used for the purposes of this example was either hydrogen or a CO/H₂ mixture that has the following percentage by weight: Hydrogen 55-65% and carbon monoxide 30-35%.

The nozzles 900, 910, and 920 are angled prior to use within the mixing chamber 330 by use of adjustment nuts 930, 940 and 950, depending on the volume, density and composition of the cooled furnace exhaust gas being mixed with the Post-combustion gas. The optimum burning is judged by the intensity of the roaring sound emanating from the post combustion reaction. The efficiency of the combustion process improves as the intensity of the roaring sound increases.

Care must be taken in adjusting the nozzles and furnace exhaust gas flow rate to ensure that the furnace exhaust gas has been cooled such that no furnace exhaust gas in proximity to any of the nozzles 900, 910 and 920 is above the Post-combustion gas ignition temperature, and for a safety margin no more than 395 K.

The mixture ratio and flow rates of Post-combustion gas and furnace exhaust gas into the mixing chamber is not fixed and depends on the type of waste product being burned. The ratios and flow rates would be increased or decreased to achieve the most intense audible ‘roar’.

The mixed gases exit the mixing chamber via the outlet 350 and enter the reducer 690. The platinum spark plug 700 is continuously sparking and provides an ignition source for the mixed gases.

The mixed gases ignite and expand into the combustion expansion chamber 360. This ignition reaction is exothermic and produces considerable heat. The ceramic lining 710 acts as a thermal barrier, preventing critical damage to the 300 mm NB SCH10 T304L welded pipe 720. The combusted mixed gases become exhaust gas.

The exhaust gas is driven to the tubular heat exchanger 370 and enters via the exhaust gas inlet 380 into the exhaust gas passage 750.

Water is introduced into the water jacket 760 via steam line inlet 400 from the steam supply line 420 and the water supply line 430, driven by water compressor pump 260 and electrical water pump 290, respectively.

The exhaust gas in the gas passage 750 is cooled by the water in the water jacket 760. The water in the water jacket 760 is heated to steam through this cooling process.

Steam leaves the water jacket 760 via the line outlet 410 and travels through the exhaust steam line 411. The steam generator connection flanges 412, 415 and 417 connected to the exhaust steam line 411 supply steam to connected steam driven electrical generators (not shown) that generate electricity.

Cooled exhaust gas leaves the heat exchanger 370 via exhaust gas outlet 390 and passes through U-bend pipe 450 to enter the matter collection chamber 460 and flows along the gas passage 1200 towards the combustion exhaust chamber inlet 140.

Ionised and/or magnetised materials in the exhaust gas in the gas passage 1200 are magnetically attracted to the three electromagnets 1210, 1220, 1230 that have a 240V A/C supply applied. The ionised and/or magnetised material enters the water tray 1250 that has water in it and this prevents escape of the ionised and/or magnetised material once the 240V A/C supply is switched off.

The exhaust gas leaves the matter collection chamber 460 via the combustion exhaust chamber inlet 140 into the combustion exhaust chamber 130. Some gas is supplied to generators via generator connections 160, 170 and 180. A further quantity of remaining exhaust gas entering the combustion exhaust chamber 130 via inlet 140 passes through the furnace return 190 and furnace return pipes 560 and 570 and into the lower end of furnace combustion chamber 530 and acts as a heated combustion gas to aid in furnace efficiency.

Another quantity of the remaining exhaust gas entering the combustion exhaust chamber 130 via inlet 140 is exhausted to the atmosphere via outlet 150.

Experimental Results H₂/CO

Testing of the efficacy of the post-combustion apparatus and process was conducted by an independent testing laboratory, SIMTARS (ABN 59 020 847 551, based in Queensland Australia). The laboratory assessed the efficiency of the Combustible Gas System in reducing air emissions including general gases (CO, CO2, NOx, total VOCs and H2S) and particulate matter (PM) when burning mixed waste materials.

It was found that the post-combustion apparatus started most easily if not exposed to furnace emissions when starting up from cold. Emissions added after the post-combustion apparatus had already started running helped to prevent fouling of the spark plug 700. An oxyacetylene pilot can be used to initiate the post-combustion apparatus if the spark plug 700 becomes fouled. The spark plug 700 is defouled by the post-combustion process when at temperature.

The mixed waste materials in the upstream furnace 500 during testing were: tyres and other rubber materials, plastics, a small lead battery, polystyrene/packaging foam, coal, rags soaked in sump oil and other general waste items.

Removal efficiency was calculated by comparing untreated baseline emissions freely flowing through the post-combustion apparatus with the post-combustion gases and to those obtained when the post-combustion apparatus was used with a post-combustion gas, being a CO/H₂ mixture of: Hydrogen 55-65% and carbon monoxide 30-35% gases. Results of the testing are set out in Table 2.

The impeller 600 was driven at 50 Hz for this testing.

Testing parameters were conducted in accordance with various standards, as set out in Table 1.

TABLE 1 Test methods Test ISO Com- Parameter Method Equivalent Analysis ments NAT A Sample plane AS 4323.1 ISO9096 1 A, B Yes criteria Gas velocity USEPA ISO10780 1 Nil Yes and Method 2 Stack gas USEPA — 1 Nil Yes density Method 3 Oxygen & carbon USEPA — 1 B Yes dioxide Method Stack gas water USEPA — 1 Nil Yes vapour Method 4 Particulate AS 4323.2 ISO9096 1 A, B Yes matter- total Oxides of USEPA — 1 C Yes nitrogen- as NO2 Method Carbon monoxide USEPA — 1 C Yes Method Volatile organic USEPA — 1 Nil Yes compounds Method Hydrogen USEPA — 1 Nil Yes Sulphide Method

TABLE 2 Test results CO/H₂ post-combustion gas Test Variation Release Point Result Test Result from Unit of Parameter Baseline using Post- Baseline Measure Sampling Time 16 32 n/a min Average exhaust 2.40 4.19 +76% m/sec velocity Average exhaust 72 305 +323%  ° C. temperature Moisture Content 15 16  +9% % Stack volume 3.6 3.7  +5% Nm³/min flow rate Carbon Dioxide 3.7 6.4 +76% vol-% Percentage Oxygen Percentage 16.8 15.5  −8% vol-% Carbon Monoxide 2,250 44 −98% mg/Nm³ Nitrogen Oxides 222 57 −74% mg/Nm³ (NOx as NO2) Particulate 0.48 0.03 −94% g/min Emission Rate TSP (total solid 158.8 8.9 −94% mg/Nm³ particulate matter) TVOC (Propane) 103.8 36.5 −65% mg/Nm³ TVOC Emission 0.32 0.11 −64% g/min Rate H2S <1.52 <1.52 n/a mg/Nm³

At the end of the test, what remained in the furnace 500 was several handfuls of white ash/carbonaceous materials, lead from the battery and metal wires left from the tyres.

FIG. 10 shows the baseline emissions for some of the parameters in Table 2 over a period of time. FIG. 11 shows the post-combustion emissions for some of the parameters in Table 2 over a period of time.

Variations in the emissions shown in both FIG. 10 and FIG. 11 are due to the heterogeneous nature of the materials burned in the furnace 500. Note that the scales for the parts per million (ppm) measurements in FIG. 10 and FIG. 11 are different.

Experimental Results H₂

Further testing was conducted to demonstrate the efficacy of the post-combustion apparatus with a different post-combustion gas, hydrogen.

For the following tests, a Testo 330i LX Advanced flue gas analyzer kit was used to obtain the results from the exhaust stack. Due to issues with fouling of the sensor, baseline figures could not be obtained, but these are expected to be similar to those obtained during the earlier testing in Table 2.

Table 3 shows the results from this testing. Results were taken when the results stabilised.

TABLE 3 Stack temp ° C. O2 % CO ppm CO2 % Furnace Fuel 416 15 160 3.5 small piece of polyethylene terephthalate Plastic bottle 384 13.7 102 4.5 Full terephthalate plastic bottle 409 14 96 3.95 Rubber tyre (small piece) 409 13 80 4.48 Rubber tyre (large piece) 465 12 61 5 triple previous rubber quantity (large load)

Counter-intuitively, the post-combustion process performed progressively better the more emissions that were released from the furnace 500. The CO value dropped when a complete plastic bottle was added to the furnace 500. Likewise, pieces of a vehicle tyre caused better results the more that was added to the furnace.

While it was not possible to get baseline quantitative emissions data from the stack, when the post-combustion process was disengaged while the furnace 500 was burning rubber tyre, the factory where the testing was being conducted quickly filled with noxious black smoke to such a degree that is was not possible to make out visual details more than a few metres away. This required an evacuation of the building. In contrast, when the post-combustion process was running, the emissions were clear and testing personnel could comfortably remain in the factory.

At 50 Hz, post-combustion was taking place in the mixing chamber 330 instead of in the combustion expansion chamber 360. This was expected behaviour as hydrogen gas has less inertia than the comparatively heavier CO/H₂ gas used in earlier testing.

The impeller 600 was driven at 60 Hz for this testing resulting in a higher flow rate than the CO/H₂ testing in Table 2. At this higher flow rate, combustion correctly took place in the combustion expansion chamber 360.

The flow rate of the exhaust at the stack was 3.36 Nm³/min, slightly higher than that in the testing results in Table 2 as a result of the increase in the impeller speed 600. 0.54 Nm³/min of hydrogen gas was being introduced into the mixing chamber 330 in the final test in Table 3.

Additional testing was conducted where the matter collection chamber 460 was inoperative by having the water tray 1250 dry and the electromagnets 1210, 1220, 1230 inoperative. The results showed an increase of carbon monoxide emissions to about 800 ppm-1,000 ppm, which is considerably above the less than 100 ppm expected from earlier testing but much lower than baseline readings of 2,250 ppm found in Table 2.

Smoke emissions from the furnace 500 at the time the matter collection chamber 460 was inoperative were relatively low due to most of the furnace fuel having been burned compared to earlier testing and based on the earlier results showing that the higher the concentration of emissions increase efficiency of the post-combustion process, this also contributed to the higher emissions.

Additional Qualitative Tests and Modifications Made for Testing Purposes

Further qualitative tests were conducted where the carbon monoxide output values were monitored showed that increasing the nozzle pressure but decreasing the nozzle aperture increased efficiency. Decreasing the number of nozzles made the post-combustion process less efficient.

The post-combustion process has been run using an oxy-acetylene pilot light instead of the spark plug 700 without significant change to the results obtained.

The use of two or three spark plugs 700 spaced circumferentially around reducer 690 has also slightly increased the efficiency of the post-combustion process, especially in its cold start-up phase.

The impeller has been allowed to be free-running once post-combustion has started and is at its operating temperature. In the case of CO/H₂, the post-combustion process drew through enough material to function adequately. A free-running impeller when using hydrogen gas is contra-indicated.

It will be appreciated by workers in the relevant field that modifications to the above examples can be made that will still fall within the scope of the present invention.

It will be appreciated that the invention broadly consists in the parts, elements and features described in this specification, which when compared to prior art relating to the field, should serve to illustrate the novelty of the invention described herein.

INDUSTRIAL APPLICABILITY

The present invention is applicable to industry, and particularly to industries that produce gaseous emissions that need to be processed into less harmful forms prior to release into the environment. There are many industries that produce such gases and there are often regulatory requirements for the reduction of toxic or environmentally damaging gaseous emissions. Additionally, industrial processes produce gases suitable for a post-combustion gas fuel, such as hydrogen or carbon monoxide and hydrogen, potentially permitting synergies between industries. This invention assists in meeting at least some regulatory requirements for the release of gaseous emissions into the environment. 

1. A post combustion apparatus comprising: a) a furnace flue inlet that (in use) connects to a furnace and permits ingress of furnace exhaust gas into the post combustion apparatus, thereby defining (in use) an extreme upstream location of furnace exhaust gas entering the apparatus; b) a post combustion exhaust chamber comprising an inlet and an outlet, the outlet defining (in use) the extreme downstream location of processed furnace exhaust gas exiting the apparatus, such that gas flows (in use) between said extreme upstream location and said extreme downstream location; c) a cooler comprising an inlet, connected to the furnace flue inlet, an outlet and a cooling element; d) a mixing chamber comprising an inlet, connected to the outlet of the cooler, an outlet, and a post-combustion gas fuel injection port located downstream of the mixing chamber inlet that, in use, introduces and mixes post-combustion gas fuel with furnace exhaust gas; e) a non-return valve interposed between the cooler outlet and the mixing chamber inlet, which non-return valve is configured to permit the flow of gas substantially in one direction only from the cooler to the mixing chamber; f) a combustion expansion chamber comprising an inlet, connected to the mixing chamber outlet, and an outlet connected to the combustion exhaust inlet; g) an igniter located downstream of the fuel injection port within the mixing chamber or the combustion expansion chamber; h) a gas power system connected to the post combustion apparatus configured to, in use, drive furnace exhaust gas and particulates from the furnace flue inlet downstream through the post combustion apparatus and to the post combustion exhaust outlet; i) wherein a mode of cross-sectional combustion expansion chamber area, bounded by internal walls of the combustion expansion chamber perpendicular to the gas flow, is larger than a mode of cross-sectional mixing chamber area, defined by internal walls of the mixing chamber and exhaust perpendicular to the gas flow; and j) wherein a mode of a cross-sectional combustion exhaust chamber area, bounded by internal walls of the combustion exhaust chamber perpendicular to the gas flow, is larger than the mode of cross-sectional mixing chamber area.
 2. A post combustion apparatus as claimed in claim 1, wherein the ratio of the mode of cross-sectional area of the combustion expansion chamber is greater than that of the mode of cross-sectional area of the mixing chamber.
 3. A post combustion apparatus as claimed in claim 1, wherein at least double that of the mode of cross-sectional area of the mixing chamber.
 4. A post combustion apparatus as claimed in claim 1, wherein the mode of a cross-sectional combustion exhaust chamber area to be at least double that of the mode of the mixing chamber area.
 5. A post combustion apparatus as claimed in claim 1, wherein the post combustion exhaust chamber outlet is connected to an exhaust flue stack.
 6. A post combustion apparatus as claimed in claim 1, wherein the exhaust path between the furnace and the exhaust stack is sealed from the air such that no additional oxygen can be introduced into the system.
 7. A post combustion apparatus as claimed in claim 1, wherein the cooling element is a steam-line heat exchanger.
 8. A post combustion apparatus as claimed in claim 1, wherein the mixing chamber is between 0.3 m and 1.5 m in length.
 9. A post combustion apparatus as claimed in claim 1, wherein the mixing chamber is between 0.8 m and 1.5 m in length.
 10. A post combustion apparatus as claimed in claim 1, wherein the post-combustion gas fuel injection port has at least one nozzle within the chamber.
 11. A post combustion apparatus as claimed in claim 10, wherein the at least one nozzle is angled to, in use, swirl post-combustion gas fuel at least partially radially perpendicular to the flow direction of the furnace exhaust gas.
 12. A post combustion apparatus as claimed in claim 1, wherein there are three post-combustion gas fuel injection ports with nozzles.
 13. A post combustion apparatus as claimed in claim 12, wherein the fuel injection ports are spaced 0.1-0.3 m apart extending in the direction of propagation of the furnace exhaust gas.
 14. A post combustion apparatus as claimed in claim 10, wherein the at least one nozzle is angled to swirl the post-combustion gas fuel in the general downstream direction.
 15. A post combustion apparatus as claimed in claim 12, wherein one of the nozzles is directed in a direction oblique to the other nozzles to impart turbulence.
 16. A post combustion apparatus as claimed in claim 10, wherein the angle of the at least one nozzle is capable of being varied.
 17. A post combustion apparatus as claimed in claim 1, wherein the combustion expansion chamber is internally ceramic lined.
 18. A post combustion apparatus as claimed in claim 17, wherein the combustion expansion chamber is internally cast ceramic lined.
 19. A post combustion apparatus as claimed in claim 17, wherein the combustion expansion chamber is internally lined using a Kaolin ceramic clay.
 20. A post combustion apparatus as claimed in claim 1, wherein the igniter is located proximal the inlet of the combustion expansion chamber.
 21. A post combustion apparatus as claimed in claim 1, wherein the igniter is a pilot light, a spark plug, a series of spark plugs or combinations of these.
 22. A post combustion apparatus as claimed in claim 21, wherein the igniter is a platinum spark plug.
 23. A post combustion apparatus as claimed in claim 21, wherein the igniter is three spark plugs.
 24. A post combustion apparatus as claimed in claim 1, wherein a matter collection chamber is installed between the combustion expansion chamber and the post combustion exhaust chamber, which matter collection chamber comprises a gas passage and a matter collection vessel.
 25. A post combustion apparatus as claimed in claim 24, wherein the matter collection vessel has at least one magnet in close association with it.
 26. A post combustion apparatus as claimed in claim 25, wherein the magnet is at least one electromagnet.
 27. A post combustion apparatus as claimed in claim 26, wherein the matter collection vessel comprises a water tray between the exhaust flow and the at least one electromagnet.
 28. A post combustion apparatus as claimed in claim 1, wherein a U-bend pipe is installed into the apparatus.
 29. A post combustion apparatus as claimed in claim 28, wherein the U-bend pipe is located before the matter collection chamber.
 30. A post combustion apparatus as claimed in claim 1, wherein water jackets are installed between the combustion expansion chamber and the extreme downstream location.
 31. A process of post combustion including the steps of: a) feeding furnace exhaust gas through a furnace flue inlet from a furnace that permits ingress of furnace exhaust gas into the post combustion apparatus, thereby defining an extreme upstream location of furnace exhaust gas entering the apparatus; b) exhausting processed furnace exhaust gas from an outlet in a post combustion exhaust chamber comprising an inlet and the outlet, the outlet defining the extreme downstream location of processed furnace exhaust gas exiting the apparatus, such that gas flows between said extreme upstream location and said extreme downstream location; c) feeding furnace exhaust gas into a cooler comprising an inlet from the furnace flue inlet, an outlet and a cooling element and cooling the furnace exhaust gas; d) feeding cooled furnace exhaust gas into a mixing chamber comprising an inlet, connected to the outlet of the cooler, an outlet, and a post-combustion gas fuel injection port located downstream of the mixing chamber inlet and mixing the cooled furnace exhaust gas with post-combustion gas fuel; e) preventing backflow of gas by passing gas through a non-return valve interposed between the cooler outlet and the mixing chamber inlet, which non-return valve is configured to permit the flow of gas substantially in one direction only from the cooler to the mixing chamber; f) passing the mixed cooled furnace exhaust gas and post-combustion gas fuel into a combustion expansion chamber comprising an inlet, connected to the mixing chamber outlet, and an outlet connected to the combustion exhaust inlet; g) igniting the mixed cooled furnace exhaust gas and post-combustion gas fuel using an igniter located downstream of the fuel injection port within the mixing chamber or the combustion expansion chamber, h) driving the gas in the post combustion process by use of a gas power system connected to the post combustion apparatus that drives gas from the furnace flue inlet downstream through the post combustion apparatus and to the post combustion exhaust outlet; i) wherein the combusting cooled furnace exhaust gas and post-combustion gas fuel mixture is free to expand through the combustion expansion chamber due to the combustion expansion chamber having a mode of cross-sectional combustion expansion chamber area, bounded by internal walls of the combustion expansion chamber perpendicular to the gas flow, is larger than a mode of cross-sectional mixing chamber area, defined by internal walls of the mixing chamber and exhaust perpendicular to the gas flow; and j) wherein the combusted cooled furnace exhaust gas and post-combustion gas fuel mixture is free to exit the combustion expansion chamber due to the combustion expansion chamber having a mode of a cross-sectional combustion exhaust chamber area, bounded by internal walls of the combustion exhaust chamber perpendicular to the gas flow, is larger than the mode of cross-sectional mixing chamber area.
 32. A process of post combustion as defined in claim 31, wherein the combustion exhaust chamber outlet is connected to an exhaust flue stack in fluid communication with an inlet for the furnace such that at least some processed furnace exhaust gas is recycled into the furnace.
 33. A process of post combustion as defined in claim 31, wherein oxygen levels in the mixing chamber are below atmospheric levels.
 34. A process of post combustion as defined in claim 33, wherein the exhaust path between the furnace and the exhaust stack is sealed from the air and no additional oxygen is introduced into the system.
 35. A process of post combustion as defined in claim 31, wherein the exhaust path minimises back-pressure by being at least the same cross-sectional area as the expansion chamber.
 36. A process of post combustion as defined in claim 31, wherein at least some processed furnace exhaust gas is used as a heat source for generators.
 37. A process of post combustion as defined in claim 31, wherein furnace exhaust gas is cooled to between 360 K and 395 K by the cooler.
 38. A process of post combustion as defined in claim 31, wherein the post-combustion gas fuel is swirled within the mixing chamber at least partially radially perpendicular to the flow direction of the furnace exhaust gas.
 39. A process of post combustion as defined in claim 31, wherein the post-combustion gas fuel is a gas capable of combustion in air with an air flame temperature of at least 1,950° C. at STP.
 40. A process of post combustion as defined in claim 39, wherein the post-combustion gas fuel is selected from the group consisting of propane, butane, methane and propane-butane mixtures.
 41. A process of post combustion as defined in claim 31, wherein the post-combustion gas fuel is a gas capable of combustion in air with an air flame temperature at STP of at least 2,000° C.
 42. A process of post combustion as defined in claim 41, wherein the post-combustion gas fuel is selected from the group consisting of a CO/H₂ mixture (Hydrogen 55-65% and carbon monoxide 30-35%), hydrogen, acetylene, propane, cyanogen and dicyanoacetylene.
 43. A process of post combustion as defined in claim 31, wherein the post-combustion gas fuel has an ignition temperature in air at STP greater than 480° C.
 44. A process of post combustion as defined in claim 43, wherein the post-combustion gas fuel is a CO/H₂ mixture (Hydrogen 55-65% and carbon monoxide 30-35%) or hydrogen.
 45. A process of post combustion as defined in claim 31, wherein the furnace exhaust gas has been cooled and mixed sufficiently that no furnace exhaust gas in proximity to the nozzle is above the Post-combustion gas ignition temperature.
 46. A process of post combustion as defined in claim 45, wherein, the furnace exhaust gas has been cooled and mixed sufficiently that no furnace exhaust gas in proximity to the nozzle is above 395 K.
 47. A process of post combustion as defined in claim 31, wherein the angle of the nozzles is capable of being varied and the nozzles are adjusted to achieve optimum burning based on an increasing roaring sound emanating from the post combustion reaction.
 48. A process of post combustion as defined in claim 31, wherein a matter collection vessel collects particulates downstream of the combustion expansion chamber, which particulates are drawn to the vessel by an electromagnetic field and captured by a water bath.
 49. A process of post combustion as defined in claim 48, wherein turbulence of the combusting cooled furnace exhaust gas and post-combustion gas fuel mixture prior to the matter collection vessel is increased.
 50. A process of post combustion as defined in claim 31, wherein the combusting cooled furnace exhaust gas and post-combustion gas fuel mixture is cooled by contact with water jackets between the combustion expansion chamber and the extreme downstream location such that the combusted cooled furnace exhaust gas and post-combustion gas fuel mixture is cooled within 2 seconds so that the gas exits the outlet of the apparatus at a temperature lower than 500° C. 